MIL-DTL-83538D
3.29 Ozone. When tested as specified in 4.6.25, the connectors shall show no evidence of cracking of
dielectric material or other damage due to ozone exposure that will adversely affect performance.
3.30 Fluid immersion. When tested as specified in 4.6.26, connectors shall meet the requirements for
3.30.1 Retention system fluid immersion. When tested as specified in 4.6.27, the insert assemblies
shall meet the requirements of contact retention (see 3.18). Effects of the fluids on resilient sealing
members shall not be a consideration of this test.
3.31 Contact walkout. When tested as specified in 4.6.28, contacts shall not become dislodged from
their normal position.
3.32 Installing and removal tool abuse. Qualifications only. When tested as specified in 4.6.29, there
shall be no evidence of damage to the contacts, the connector insert, or the contact retaining mechanism.
3.33 High temperature exposure. See 4.6.30.
3.33.1 High temperature exposure with contact loading. When tested as specified in 4.6.30.1, the
contacts shall maintain their specified locations as shown (see 3.1) and there shall be no electrical
discontinuity.
3.33.2 High temperature exposure for connectors. When tested as specified in 4.6.30.2 for 1,000
hours, connectors shall perform satisfactorily and pass succeeding tests in the qualification test
sequence.
3.34 Electrolytic erosion. When tested as specified in 4.6.31, pin contacts shall show no exposure of
base metal due to electrolytic erosion. Corrosion deposits shall not be considered as defects.
3.35 Icing and freezing rain. When tested as specified in 4.6.32, the connector assembly shall
withstand the icing and freezing rain environment (sea spray condition) specified in 4.6.32. The force
required to separate the connector shall not exceed 334 Newtons (75 pounds).
3.36 Sand and dust. When tested as specified in 4.6.33, the connector assembly shall withstand the
blowing dust and blowing sand conditions of MIL-STD-810, method 510. Blowing dust air velocity shall
be 8.9 meters/second minimum. The blowing sand air velocity shall be 29 meters/second minimum with
a sand concentration of 2.2 ±0.5 grams/cubic meter. Immediately following this exposure, the coupling
force and decoupling force shall not exceed the requirements specified herein (see 3.8.2 and 3.8.3) by
more than 25 percent.
3.37 Launcher drive pin strength. Applies to MIL-DTL-83538/4 receptacle only. When tested as
specified in 4.6.36, the launcher drive pins shall show no evidence of permanent deformation or damage
such as would impair the operation of the connector or launcher mechanism.
3.38 Lightning strike. Not applicable to the MIL-DTL-83538/11 buffer plug. The connector set shall
show no damage or degradation in performance, including seizing, pitting, or damage to the insulation of
the connector when subjected to the lightening strike requirements specified in 4.6.38. Connectors shall
be mated and unmated in accordance with the requirements of 3.8.1 and 3.8.3 without recourse to tools,
except for MIL-DTL-83538/12. Failure to unmate the connectors because they have welded together
shall constitute a test failure.
15
For Parts Inquires submit RFQ to Parts Hangar, Inc.
© Copyright 2015 Integrated Publishing, Inc.
A Service Disabled Veteran Owned Small Business